Tohoku University
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
Department of Aerospace Engineering, Graduate School of Engineering, Tohoku University
JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010
巻
JAXA-SP-10-012
発行年
2011-02-28
会議概要(会議名, 開催地, 会期, 主催者等)
第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP)
会議概要(会議名, 開催地, 会期, 主催者等)(英)
42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25, 2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan
抄録(英)
An all-speed scheme, SLAU(Simple Low-dissipative AUSM) was implemented into the cartesian mesh Euler solver using Building-Cube Method for a flow-field with a wide range of speeds. Its validation was conducted with ONERA M6 wing and ROBIN (ROter Body INteraction) fuselage.
内容記述
形態: カラー図版あり
内容記述(英)
Physical characteristics: Original contains color illustrations